Zobrazeno 1 - 10
of 17
pro vyhledávání: '"Zurriati Mohd Ali"'
Publikováno v:
Malaysian Journal of Computing, Vol 8, Iss 1, Pp 1301-1310 (2023)
The aircraft with a vertical take-off and landing (VTOL) technology has been widely studied all around the world as it is one of the most advanced systems that could be used by modern aircraft. It was invented for any types of simple multirotor aircr
Externí odkaz:
https://doaj.org/article/b0777f9010e843d6bed03d2ca466f323
Autor:
Kamariah Md Isa, Ainaa Maya Munira Ismail, Zurriati Mohd Ali, Mohammad Abdullah, Fazila Mohd Zawawi
Publikováno v:
Journal of Advanced Research in Fluid Mechanics and Thermal Sciences. 87:148-171
Presently the worldwide lockdown from Covid-19 give a huge effect on different sectors across the board, notably on energy consumption. Lockdowns have fuelled the intensification of low-carbon resources in terms of electricity production, yet a drast
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::021fa34e3f50a7c0b6e19ee1ff81c3a3
https://doi.org/10.37934/arfmts.87.3.148171
https://doi.org/10.37934/arfmts.87.3.148171
Autor:
Zurriati Mohd Ali, Nik Izwan Kamel, Noor Iswadi Ismail, Ahmad Aliff Ahmad Shariffuddin, Mahamad Hisyam Mahamad Basri, Hazim Sharudin
Publikováno v:
Journal of Advanced Research in Fluid Mechanics and Thermal Sciences. 84:50-62
This paper presents the investigation and improvement of lift and drag characteristics of Neo-Ptero micro-UAV models based on the virtual wind tunnel method. Despite its successful development and flight stability, the lift and drag coefficients char
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::64c6f6ad07524a11fc5008bbe0858f75
https://doi.org/10.37934/arfmts.84.2.5062
https://doi.org/10.37934/arfmts.84.2.5062
Publikováno v:
Journal of Advanced Research in Fluid Mechanics and Thermal Sciences. 77:124-131
Paper plane has a high potential to be upgraded as a Micro Air Vehicle (MAV). Due to its simplicity, paper plane offers easier design option compared to the biological inspired designs as shown in recent MAV development. However, researchers have und
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c10297b7154acd70af3bd64de92c84ed
https://doi.org/10.37934/arfmts.77.1.124131
https://doi.org/10.37934/arfmts.77.1.124131
Autor:
Zurriati Mohd Ali, Wirachman Wisnoe, Ehan Sabah Shukri Askari, Nornashiha Mohd Saad, Rizal Effendy Mohd Nasir
Publikováno v:
MATEC Web of Conferences, Vol 256, p 02004 (2019)
This paper presents an aerodynamic characteristic study in longitudinal direction of UiTM Blended Wing Body-Unmanned Aerial Vehicle Prototype (BWB-UAV Prototype) equipped with horizontal stabilizers. Flight tests have been conducted and as the result
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::b1d7297f19fa2b7f53907ab5d3a51c6e
https://doaj.org/article/77c3bc74081e43c0b511450962018cf5
https://doaj.org/article/77c3bc74081e43c0b511450962018cf5
Autor:
Wirachman Wisnoe, Zurriati Mohd Ali, Wahyu Kuntjoro, Iskandar Shah Ishak, N. Ahmad, M. Z. Katon
Publikováno v:
IOP Conference Series: Materials Science and Engineering. 834:012015
Blended Wing Body Aircraft (BWB) is an unconventional aircraft that combined the conventional and flying wing aircraft’s design. The unique design of the BWB offers a high fuel efficiency, low noise, and large payload volume for the size of aircraf
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::77d18ff1385d57e17e0b76c0fae7af67
https://doi.org/10.1088/1757-899x/834/1/012015
https://doi.org/10.1088/1757-899x/834/1/012015
Publikováno v:
Applied Mechanics and Materials. 225:38-42
This paper presents a study on the effect of canard setting angle on the aerodynamic characteristic of a Blended Wing Body (BWB). Canard effects to BWB aerodynamic characteristics are not widely investigated. Hence the focus of the study is to invest
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::cf15e5314ff080cf0e1958a8bcd3d056
https://doi.org/10.4028/www.scientific.net/amm.225.38
https://doi.org/10.4028/www.scientific.net/amm.225.38
Publikováno v:
Advanced Materials Research. :6636-6640
The objective of this paper is to investigate longitudinal flight dynamics of the said aircraft at loitering flight condition near sea level. Three mathematical dynamic models are used to compute transient response of Baseline-II E-2 BWB along with a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e9b2bc3353d33c1bab990e59003267ee
https://doi.org/10.4028/www.scientific.net/amr.433-440.6636
https://doi.org/10.4028/www.scientific.net/amr.433-440.6636
Autor:
Wan Khairuddin Wan Ali, Norazila Othman, Tholudin Mat Lazim, Wan Zaidi Wan Omar, Shuhaimi Mansor, Zurriati Mohd Ali, Ainullotfi Abdul-Latif, Mastura Abd Wahid, Mohd. Nazri Bin Nasir, Shabudin Mat, Muhammad Zaki Bin Abdul Manaf, Md. Nizam Dahalan
Publikováno v:
International Review of Mechanical Engineering (IREME). 12:263
This paper discusses the impact of the external store on the aerodynamic performance of the light aircraft model in the subsonic region. Light aircrafts are commonly used for pilots training, survey, leisure and transportation. To date, there have be
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3966ef972b7c9b81803b823279c7dc47
https://doi.org/10.15866/ireme.v12i3.13574
https://doi.org/10.15866/ireme.v12i3.13574
The aerodynamics characteristics of a blended-wing body (BWB) aircraft were obtained in Universiti Teknologi MARA low speed wind tunnel. The scaled-down of BWB model consisted of a canard as its horizontal stabilizer. There were four canards with dif
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::30d3680a7cc1e18fddb96d71159b7aec
